US4362674A

US4362674A - Process for making radiation cured silicone rubber articles

Info

Publication number: US4362674A
Application number: US06/211,252
Authority: US
Inventors: John G. DuPont; Paul A. Goodwin
Original assignee: High Voltage Engineering Corp
Current assignee: SEIP Ltd 551 MADISON AVENUE NEW YORK NY 10022 A CORP OF; Sanwa Business Credit Corp
Priority date: 1980-11-28
Filing date: 1980-11-28
Publication date: 1982-12-07
Anticipated expiration: 2000-11-28

Abstract

A process for making radiation cured silicone rubber articles is disclosed wherein a hydroxyl-terminated polysiloxane having a molecular weight from about 50,000 to about 2,000,000, optionally modified by mixing with up to 85% of an end-stopped silicone rubber, is mixed with from about 10 to about 70 parts per hundred of rubber of a finely divided silica filler with a particle size in the reinforcing range and other inlet fillers as determined by desired final properties; the composition so prepared is formed into the desired shape at room temperature; the article so formed is precured to improve the mechanical properties of the material with which it is made by exposure to ammonia gas, ammonium hydroxide, or to the vapors or solutions of a volatile amine at room temperature; and the precured article is irradiated with high energy electrons or gamma radiation to effect a permanent cure of the material from which the article is formed.

Description

BACKGROUND

I. Field of Invention

The present invention relates to processes for making radiation cured silicone rubber articles, and, in particular, to a process wherein articles formed of silicone rubber are treated substantially immediately after their formation to withstand without serious deformation the stresses involved in the mechanical handling necessary to convey such articles through irradiation apparatus.

II. Summary of the Prior Art

Unlike some of the organic rubbers, particularly the newer thermoplastic rubbers, silicone rubber must be crosslinked or vulcanized in order to have useful properties. The cross-linking process is usually referred to, in the case of silicone rubber as "cure" or "curing." Since the invention of silicone rubber, the cure has been done by incorporating free radical producing catalysts, typically organic peroxides or azo compounds, mixed with rubber and heating the composition to a high temperature, typically 150°-250° C., for periods ranging from a few minutes to several hours.

Virtually all commercial, heat-cured silicone rubbers today are cured with organic peroxides such as benzoyl peroxide, dichlorobenzoyl peroxide, tert-butyl perbenzoate or dicumyl peroxide. However, products cured by such curing agents all suffer from a disadvantage in that, after cure has been completed, the products contain chemical residues from the decomposition of the peroxide, and these residues tend to affect deleteriously properties such as heat-ageing, electrical resistivity and reversion resistance. The presence of these residues, moreover, limits the use of otherwise biologically inert silicone rubber products in medical applications, since the residues tend to be leached out of the rubber by body fluids, saline solutions and other liquid products used in medicine.

There are other problems of peroxides curing catalysts. One is that they are very sensitive to catalyst "poisons" and many common rubber compounding ingredients, which otherwise would be included in silicone rubber to improve physical strength, flame retardancy, thermal ageing, and so on, cannot be used because they prevent or retard the peroxide cure. For example, most reinforcing carbon blacks, commonly used in organic rubbers, completely prevent peroxide cure of silicones. Certain peroxide residues, being volatile, cause porosity in the cured rubber and others tend to diffuse out of the compound forming unsightly oily films or crystals on the surface.

More recently, liquid silicone rubbers have been introduced to the market, which cure by other mechanisms to solid, vulcanized rubber products. These liquid rubbers (which occasionally are pastes or semi-solids) typically cure at room temperature, or at relatively low temperatures, and are categorically referred to as "Room Temperature Vulcanizing" (RTV) silicone rubbers. There are several mechanisms for curing RTV rubbers. Some contain crosslinking agents which are activated by atmospheric moisture and others are cured by complex catalysts containing platinum salts. All of them yield chemical byproducts from the curing reaction, some of them relatively toxic chemicals such as organic amines, acetic acid or methanol. They all, therefore, suffer from the disadvantages cited for peroxide cure, above.

It has long been known that these disadvantages can be avoided, and that cured silicone rubber parts free of deleterious catalyst residues can be obtained, by irradiation with high energy electrons or gamma rays, to effect the cure. For example, the curing of silicone rubber with electrons was disclosed and claimed in U.S. Pat. No. 2,763,609 to Lewis, et al. This curing process and the benefits resulting therefrom are discussed in detail in that patent, the disclosure of which is incorporated herein by reference. In spite of the significant advantages of the irradiation curing process, however, it has never been commercialized, to the best of our knowledge, because of a serious obstacle to production of commercial quantities of formed, irradiated silicone parts. The problem is that Silicone rubber, like other curable polymers, must usually be formed into the desired, final shape before cure because, after cure, it is crosslinked and, therefore, not formable by the usual processes such as molding, extrusion, or casting.

Yet unlike most other polymers, silicone rubber is almost completely lacking in physical strength before cure. Uncured silicone rubber is extremely soft, easily deformed even by working with the bare hands, and it flows readily under low pressures, such as might be experienced when winding a silicone tube or sheet on a reel. Cure, whether by peroxide catalysts or by irradiation, improves the physical strength of silicone rubber dramatically. Tensile strength, for example, is increased 20-50 times.

Because of its low precure strength (referred to in the trade as "green strength"), it is impossible to convey extruded silicone tubing, or extruded silicone insulated wire, for example, from the extruder to the radiation vault, and to convey it under the electron beam repeatedly, without serious physical damage. If the silicone rubber is to be formed by molding, it is nearly impossible to remove it from the mold without damage, in order to irradiate it. Of course, it cannot be radiation-cured while still in the mold, at least by electron irradiation, because the electrons cannot penetrate the thick metal walls of a typical mold. This problem has prevented commercialization of the radiation cure process.

SUMMARY OF THE PRESENT INVENTION

It is, therefore, an object of this invention to provide a practical process for curing silicone rubber formed objects by the use of high energy radiation and, particularly, by the use of high energy electrons.

It is a further object to cure silicone rubber without the use of heat energy, and without the use of chemical agents or catalysts which leave deleterious residues in the rubber.

A still further object is to effect an apparent cure of silicone rubber formed objects, immediately after the forming process, so that they can be handled, stored and conveyed through irradiation equipment without physical damage.

The present invention is based on the unexpected discovery that a compound of a silicone rubber at least 15% of which has, predominantly, silanol end groups, and a finely divided silica filler with a particle size in the reinforcing range, is strengthened markedly by a brief exposure, at room temperature, to ammonia gas, or ammonium hydroxide, or to the vapors or solutions of a volatile amine. Although it seems likely (although not proven) that this strengthening does not result from permanent, chemical crosslinking, but is, rather, an apparent and somewhat transient cure, the increase in mechanical properties obtained is more than adequate to enable the formed object, whether it be an extruded tube, wire insulation, thin sheet or molded object, to withstand the severe tensile, compressive and abrasive stresses involved in the mechanical handling necessary to convey it through irradiation apparatus.

Crosslinking by irradiation with high energy electrons then introduces permanent, primary bond crosslinks. At least in the case of ammonia gas as the precure agent, the ammonia which diffuses into the compound to effect the precure seems to diffuse back out during, or soon after irradiation, and is not detectable by sensitive analytical techniques. Thus, crosslinking has been effected without leaving measurable chemical residues.

DETAILED DESCRIPTION OF A PREFERRED EMBODIMENT OF THE PRESENT INVENTION

In the preferred embodiment of the invention, a hydroxyl-terminated polysiloxane having a molecular weight from about 50,000 to about 2,000,000, optionally modified by mixing with up to 85% of an end-stopped silicone rubber polymer, is mixed with from about 10 to about 70 parts per hundred of rubber of a fumed silica. Other inert fillers may be added to obtain desired property profiles. Suitable mixing equipment includes such high shear mixers as two-roll compounding mills or sigmablade doughmixers.

The resulting compound is then formed to the desired final shape by an appropriate forming process. That is, tubes or rods are extruded through a die from a rubber extruder; wire insulation is extruded onto bare wire through a crosshead extruder; flat sheets are calendered or extruded through a slit die, and so on. Forming is normally carried out at or near room temperature.

The fabricated rubber is then conveyed immediately through an atmosphere of ammonia or amine vapors, allowing a residence time in the vapors of from about 10 seconds to about 60 minutes, depending on the sample thickness and degree of cure required. The precuring step is also preferably carried out at or about room temperature.

The fabricated rubber, which has now been strengthened greatly by the precuring process is then crosslinked by exposure to high energy radiation. High energy electrons are preferred as the radiation source, but gamma radiation may also be used. The radiation dose may be from about 1 megarad to about 50 megarads with an optimum range from 5 megarads to 20 megarads.

For silicone rubber polymers to have useful mechanical properties they must be compounded with fillers of extremely small particle size, generally less than about 50 mμ in diameter and a high surface area, generally more than 150 M² /g. This type of filler is known as a "reinforcing filler" as opposed to a filler of larger particle size and a smaller surface area which contributes little to the mechanical strength of a rubber, but rather serves primarily to reduce the cost of the compound. The reinforcing fillers used in silicone rubber are generally finely divided silicas, although carbon black fillers may also be used. The use of such "reinforcing fillers" is well known in the prior art and is described, for example, at pages 405-423 of "Reinforcement of Elastomers," edited by Gerard Kraus (Interscience Publishers, New York) in a chapter by John W. Sellers and Frank E. Toonder entitled, "Reinforcing Fine Particle Silicas and Silicates."

For the operation of this invention silica fillers are essential. Fumed silicas are preferred. Fumed or pyrogenic silica comprises a form of silica described in U.S. Pat. No. 2,888,424. Such silicas are sold under the trade designation Cabosil, by the Cabot Corporation of Boston, Massachusetts. Another type of silica known as silica aerogel, not now sold commercially, but previously sold under the trade designation Santocel by the Monsanto Chemical Company, is also effective. Silica aerogels are described, for example, in U.S. Pat. Nos. 2,657,149 and 2,093,454.

Although fumed silicas or silica aerogels, or other equally finely divided silicas are essential to the process disclosed herein, they may be used in conjunction with other inert fillers or additives conventionally used to alter specific properties, reduce cost, or as pigments. Such fillers include clays, metal oxides, carbon black, and larger particle size silicas. Fillers may be process aids (such as silicone oil and a reinforcing filler), flame retardants, pigments, stabilizers, etc. It is well known that fillers may be surface coated or otherwise treated.

In order to illustrate the improved properties attainable with this invention the following examples are presented. These examples are presented by way of disclosure only and should not be construed as being in any way limiting. In these examples SE-30 refers to a linear end-capped polydimethylsiloxane gum produced by General Electric Company; SE-33 refers to a linear end-capped polydimethyl-vinylsiloxane gum produced by General Electric Company; SE-75 refers to a linear non-end-capped polydimethylsiloxane gum produced by General Electric Company; Cabosil MS-7 refers to a pyrogenic, high surface area silica produced by the Cabot Corporation; Hisil 233 refers to a medium surface area silica produced by PPG Industries, Inc.; Imsil A-10 refers to a low to medium surface area silica produced by Illinois Minerals Company; Santocel-C refers to a silica aerogel previously produced by the Monsanto Chemical Company; and washed P.D.M.S. refers to a polydimethylsiloxane having, predominantly, silanol end-groups. The latter polymers may be made by the KOH-catalyzed polymerization of octamethylcyclotetrosiloxane as disclosed in Warrick U.S. Pat. No. 2,541,137, issued Feb. 13, 1951 and subsequent removal of potassium ions by washing the polymer with water, or by other suitable techniques. Such polymers will hereinafter be referred to as "hydroxyl-terminated polydimethylsiloxanes."

It will, of course, be understood by those skilled in the art that the reactive components are the silanol end-groups, and that the structure of the silicone chain may be varied considerably without departing from the scope of this invention. Thus, hydroxyl-terminated polysiloxanes, in which some of the methyl groups have been replaced by other aliphatic, aromatic, or cycloaliphatic radicals such as ethyl, vinyl, allyl, phenyl, etc. may also be employed. Methyl-phenyl type copolymers will probably require relatively higher dosage of irradiation. Similarly some of the methyl groups may be replaced by fluorinated, or other halogenated radicals.

The controlled precure which is obtained by exposing hydroxyl-terminated polysiloxane rubber compounds to ammonia or amines is highly specific to the hydroxyl-terminated polymer as is clearly demonstrated by the data presented hereinbelow in Example I. Most commercial silicone rubber gums are linear polysiloxanes whose molecules are terminated with trimethylsilyl or other inert groups. When compounded with a silica filler, the resulting compounds are completely unaffected by ammonia or amines. On the other hand, a KOH-catalyzed polymer, as disclosed in the Warrick U.S. Pat. No. 2,541,137, made without trimethylsilyl endgroups, and still containing the potassium ions (i.e., not water washed) develops an apparent cure rapidly, when compounded with the silica filler, to such an extent that it is difficult to form by extrusion, molding, calendering, etc.

However, it is possible to blend conventional silicone rubber polymers, endstopped with trimethylsilyl, or other monofunctional silyl groups, with the hydroxyl-terminated polysiloxane up to 85% of the mixture, and to obtain a useful degree of precure when exposed to ammonia or amine vapors.

EXAMPLE I

In the first series of experiments, various silicone polymers and fillers were mixed together at room temperature on a laboratory two-roll mill. The compounds were then stripped from the mill and pressed into 100 mil-thick sheets on a water-cooled laboratory press. The sheets were then exposed to an atmosphere of anhydrous ammonia for 10 minutes. These results are summarized in Table I.

                                  TABLE I                                 
__________________________________________________________________________
          A  B  C  D  E  F  G  H  I  J                                    
__________________________________________________________________________
SE-33     100   100                50                                     
SE-30        100                                                          
SE-75              100                                                    
                      100                                                 
                         100   100                                        
                                   50                                     
Washed PDMS                 100                                           
Cabosil MS-7                                                              
           25                                                             
              25          25                                              
                             30    30                                     
Hisil 233        25                                                       
                    25                                                    
Imsil A-10             25                                                 
Santocel-C                                                                
Tensile (psi) Prior                                                       
          Nil                                                             
             Nil                                                          
                Nil                                                       
                   Nil                                                    
                      Nil                                                 
                         Nil                                              
                            Nil                                           
                               Nil                                        
                                  Nil                                     
to NH.sub.3 Exposure                                                      
          ↓                                                        
             ↓                                                     
                ↓                                                  
                   ↓                                               
                      ↓                                            
Tensile (psi) After                                                       
          ↓                                                        
             ↓                                                     
                ↓                                                  
                   ↓                                               
                      ↓                                            
                         300                                              
                            850                                           
                               220                                        
                                  450                                     
NH.sub.3 Exposure                                                         
% Elongation After                                                        
          ↓                                                        
             ↓                                                     
                ↓                                                  
                   ↓                                               
                      ↓                                            
                         700                                              
                            750                                           
                               350                                        
                                  900                                     
NH.sub.3 Exposure                                                         
__________________________________________________________________________

EXAMPLE II

In this example various amounts of pyrogenic silica were compounded with a non-end blocked polydimethylsiloxane gum (SE-75) and cured with anhydrous ammonia for 10 minutes. These data are summarized in Table II:

              TABLE II                                                    
______________________________________                                    
              A    B      C      D     E                                  
______________________________________                                    
SE-75 Non-end Capped                                                      
                100    100    100  100   100                              
Polydimethylsiloxane                                                      
Polymer (Parts)                                                           
Cabosil MS-7 (phr)                                                        
                 15     25     30   35    45                              
Tensile After 10                                                          
                 50    300    600  1100  1300                             
Minutes' Exposure to NH.sub.3                                             
(psi)                                                                     
% Elongation After 10                                                     
                400    700    750  800   750                              
Minutes' Exposure to NH.sub.3                                             
______________________________________

EXAMPLE III

In this series of experiments, a formulation containing 100 parts of non end-capped polydimethylsiloxane gum and 40 parts of fumed silica were exposed to vapors of various organic amines for a period of 10 minutes. Tensile and elongation tests were then performed on these samples. The date are summarized in Table III.

              TABLE III                                                   
______________________________________                                    
                      TENSILE/   TENSILE/                                 
                      ELON-      ELON-                                    
                      GATION     GATION                                   
                      PRIOR TO   AFTER                                    
COMPOUND    AMINE     EXPOSURE   EXPOSURE                                 
______________________________________                                    
100 g.                                                                    
      SE-75     Methyl-   Nil       970-500                               
40 g. fumed silica                                                        
                Amine                                                     
100 g.                                                                    
      SE-75     Dimethyl- Nil      1050/550                               
40 g. fumed silica                                                        
                Amine                                                     
100 g.                                                                    
      SE-75     Trimethyl-                                                
                          Nil      1050/600                               
40 g. fumed silica                                                        
                Amine                                                     
100 g.                                                                    
      SE-75     Allyl-    Nil       900/600                               
40 g. fumed silica                                                        
                Amine                                                     
100 g.                                                                    
      SE-75     Pyridine  Nil      1050/650                               
40 g. fumed silica                                                        
______________________________________

As can be seen from this data, organic primary, secondary and tertiary amine vapors may be used to provide a pseudo-cure to the silicone rubber.

EXAMPLE IV

In this series of experiments, a formulation composed of 100 parts non-end capped polydimethylsiloxane gum and 40 parts of fumed silica were cured with anhydrous ammonia and then irradiated with high-energy electrons to specified doses. Tensile and elongation tests were performed on unaged specimens, specimens aged at 220° C. for 50 hours, and specimens aged in boiling water (100° C.) for 50 hours. These data are summarized in Table IV.

              TABLE IV                                                    
______________________________________                                    
DOSE (Mrads)                                                              
              0       2        5      10                                  
______________________________________                                    
Initial Tensile 1200      1100     850  800                               
Strength (psi)                                                            
Initial Elongation (%)                                                    
                500       420      250  125                               
Tensile After 50 Hours                                                    
                450       650      850  750                               
at 220° C. (psi)                                                   
Elongation After 50 Hours                                                 
                350       325      200   50                               
at 220° C. (%)                                                     
Tensile After 50 Hours                                                    
                <100      650      850  700                               
in Water at 100° C.                                                
Elongation After 50 Hours                                                 
                <50       450      250  100                               
in Water at 100° C.                                                
______________________________________

As can be seen from these data, a permanent cure is effected by irradiation with high-energy electrons.

EXAMPLE V

In this series of experiments, two formulations were cured with anhydrous ammonia and irradiated by high-energy electrons to the desired dose. Specimens were then subjected to compression at elevated temperatures and the % permanent set measured. These results are given in Table V.

              TABLE V                                                     
______________________________________                                    
                            COMPRESSION                                   
                            SET (%)                                       
                  DOSE      (22 HOURS                                     
FORMULATION       (MRADS)   at 175° C.                             
______________________________________                                    
100g SE-75                                                                
40g Cabosil MS-7      2         54                                        
NH.sub.3 Cure for 10 Minutes                                              
                      5         38                                        
100g SE-75                                                                
50g Cabosil MS-7      2         33                                        
NH.sub.3 Cure for 10 Minutes                                              
                      5         27                                        
______________________________________

EXAMPLE VI

In this series of experiments, a compound composed of 100 parts non-end blocked polydimethylsiloxane gum, 40 parts fumed silica (Cabosil MS-7) treated with CF-11 73 (a silicone fluid manufactured by General Electric Company) in accordance with U.S. Pat. No. 2,939,009, 40 parts non-reinforcing silica (Imsil A-10) and 2 parts red iron oxide were blended on a two-roll mill and prehardened by exposure to NH₃. The material was then permanently cross-linked by means of high energy electrons. This material, along with a conventional peroxide cured material (GE 9100-A) was then heat aged at 300° C. for 100, 250 and 350 hours. At the end of this time, physical properties were measured in order to determine the relative heat stability of these materials. These data are summarized in Table VI.

                                  TABLE VI                                
__________________________________________________________________________
                  TENSILE/ELONGATION/DUROMETER                            
            DOSE         100 HRS.                                         
                               250 HRS.                                   
                                     350 HRS.                             
COMPOUND    (MRADS)                                                       
                  INITIAL                                                 
                         AT 300° C.                                
                               AT 300° C.                          
                                     AT 300° C.                    
__________________________________________________________________________
100 parts non-end                                                         
blocked PDMS                                                              
40 parts fumed silica                                                     
40 parts non-reinforcing                                                  
silica                                                                    
2 parts Fe.sub.2 O.sub.3                                                  
            10    930/160/68                                              
                         575/135/67                                       
                               475/100/77                                 
                                     530/65/73                            
100 parts non-end                                                         
blocked PDMS                                                              
40 parts fumed silica                                                     
40 parts non-reinforcing                                                  
silica                                                                    
2 parts Fe.sub.2 O.sub.3                                                  
            20    950/100/72                                              
                         470/75/70                                        
                               465/50/85                                  
                                     515/50/80                            
Peroxide cured                                                            
polymethylvinylsiloxane                                                   
            (Peroxide                                                     
                  1000/400/55                                             
                         545/100/75                                       
                               460/0/97                                   
                                     700/0/96                             
(GE 9100-A) cure)                                                         
Peroxide cured                                                            
polymethylvinylsiloxane                                                   
            (Peroxide                                                     
                  1100/400/59                                             
                         690/75/85                                        
                               600/30/93                                  
                                     550/0/95                             
(GE SE-9058)                                                              
            cured)                                                        
__________________________________________________________________________

As can be seen from these data, silicone crosslinked by high energy electrons appears to have superior heat stability (based on % elongation) as compared to peroxide crosslinked silicone.

It will be understood that the embodiments, product, process, and practices described and portrayed herein have been presented by way of disclosure, rather than limitation, and that various modifications, substitutions, and combinations may be effected without departure from the spirit and scope of this invention in its broader aspects.

Claims

We therefore claim:

1. A process for making radiation cured silicone rubber articles comprising the steps of:

(a) forming into a desired shape a mixture of (i) silicone gum which includes a substantial amount of one or more hydroxyl-terminated polysiloxanes having a molecular weight from about 50,000 to about 2,000,000 and (ii) about 10 to about 70 parts per hundred of rubber of a finely divided silica filler with a particle size in the reinforcing range;

(b) treating the mixture so formed with a precuring agent selected from the group consisting of ammonia gas, ammonium hydroxide, vapors of a volatile amine, or a solution of a volatile amine; and

(c) irradiating with high energy ionizing radiation the precured shape.

2. The process of claim 1 wherein the silica filler is selected from the group consisting of fumed silicas and silica aerogels.

3. The process of claim 1 wherein said mixture includes up to 85% of an end-stopped silicone rubber.

4. The process of claim 1 where the irradiation is accomplished with high energy electrons to a dose from about 1 megarad to about 50 megarads.

5. The process of claim 1 wherein the radiation is gamma radiation.

6. The process of claim 4 or of claim 5 wherein the dosage is from about 5 megarads to about 20 megarads.

7. The process of claim 1 wherein said mixture includes inert fillers.

8. The process of claim 1 wherein all said steps are carried out at substantially room temperature.